Technical Papers
Mar 15, 2013

Instrumentation for Aerospace Applications: Electronic-Based Technologies

Publication: Journal of Aerospace Engineering
Volume 26, Issue 2

Abstract

Throughout the 70-year history of the National Aeronautics and Space Administration (NASA) Glenn Research Center (GRC), instrumentation engineers have provided measurement methods and devices necessary to support ongoing and future aeropropulsion research and development efforts. On occasion, routine instrumentation approaches are perfectly suited for the task at hand. However, as propulsion components and systems become more complex through the incorporation of new materials and higher temperature operation, modifications to traditional instrumentation methods or entirely new methods are necessary. This paper provides a glimpse of the core electronic-based instrumentation methods developed throughout the years to measure temperature, strain, pressure, heat flux, and chemical gas species and describes how these methods are evolving to meet the instrumentation challenges of high-performance propulsion systems. It is clear that future aeropropulsion systems will operate at higher temperatures and require more onboard electronics for health monitoring and control functions. For this reason, a significant effort in high-temperature electronics based on the wide-bandgap semiconductor silicon carbide was initiated and has demonstrated several world’s first electronic sensors and devices operating at 600°C. It is concluded that electronic-based sensors and devices will continuously be pushed to meet the needs of increasingly harsher environment measurements.

Get full access to this article

View all available purchase options and get full access to this article.

Acknowledgments

Many colleagues supported this publication effort. Interviews with retired instrumentation specialists Austin C. Herr, D. Robert Englund, Raymond Holanda, J. A. Powell, Arthur Decker, and John Pollack were especially informative and enjoyable. The contributions of Gustave C. Fralick and John D. Wrbanek are very much appreciated.

References

Blackshear, P. L., Rayle, W. D., and Tower, L. K. (1955). “Study of screeching combustion in a 6-inch simulated afterburner.” TN-3567, National Advisory Committee for Aeronautics, Washington, DC.
Chen, L. Y., and Lei, J. F. (2006). “Packaging of harsh environment MEMS devices.” MEMS design and fabrication, M. Gad-el-Hak, ed., CRC Press, Boca Raton, FL, 12-1–12-28.
Chen, L. Y., Spry, D. J., and Neudeck, P. G. (2006). “Demonstration of 500°C AC amplifier based on SiC MESFET and ceramic packaging.” Proc., Int. High Temperature Electronics Conf., International Microelectronics and Packaging Society, Washington, DC, 240.
Dawson, V. (1991). “Engines and innovation, Lewis Laboratory and American propulsion technology.” SP-4306, NASA, Washington, DC.
DeLaat, J. C., and Chang, C. T. (2003). “Active control of high frequency combustion instability in aircraft gas-turbine engines.” TM-212611, NASA, Washington, DC.
Elmore, D. L., Robinson, W. W., and Watkins, W. B. (1986). “Further development of the dynamic gas temperature measurement system.” CR-179513, NASA, Washington, DC.
Englund, D. R. (1986). “Research instrumentation for hot section components of turbine engines.” TM-88851, NASA, Washington, DC.
Englund, D. R., and Richards, W. B. (1985). “The infinite line pressure probe.” ISA Trans., 24(2), 11–19.
Evans, L. J., Okojie, R. S., and Lukco, D. (2012). “Development of an extreme high temperature n-type ohmic contact to silicon carbide.” Materials science forum, silicon carbide and related materials 2011, R. P. Devaty, M. Dudley, T. P. Chow, and P. G. Neudeck, eds., Tech Publications, Dürnten-Zurich, Switzerland, 841–844.
Fralick, G., Wrbanek, J., and Blaha, C. (2002). “Thin film heat flux sensor of improved design.” TM-2002-211566, NASA, Washington, DC.
Fralick, G. C., Decker, A. J., and Blue, J. W. (1989). “Results of an attempt to measure increased rates of the reaction 2D + 2D→3758 He + n in a nonelectrochemical cold fusion experiment.” TM-102430, NASA, Washington, DC.
Glawe, G. E., and Krause, L. N. (1974). “Miniature probes for use in gas turbine testing.” TM-X-71638, NASA, Washington, DC.
Grant, H. P., Przybyszewski, J. S., Anderson, W. L., and Claing, R. G. (1983). “Thin film strain gage development program-strain gages for dynamic measurement.” CR-174707, NASA, Washington, DC.
Gregory, O. J., Chen, X., Fralick, G. C., and Wrbanek, J. D. (2007). “Preparation and characterization of high temperature thermoelectrics based on metal oxide nanocomposites.” Proc., Materials Research Society Symp. on Thermoelectric Power Generation, T. P. Hogan, J. Yang, R. Funahashi, and T. Tritt, eds., MRS, Warrendale, PA, 1044.
Holanda, R. (1969). “Evaluation of a volume-ratio system for vacuum gage calibration from 10−8 to 10 torr.” TN D-5406, NASA, Washington, DC.
Holanda, R., Glawe, G. E., and Krause, L. N. (1974). “Miniature sheathed thermocouples for turbine blade temperature measurement.” TN D-7671, NASA, Washington, DC.
Hulse, C. O., Bailey, R. S., and Lemkey, F. D. (1985). “High temperature static strain gage alloy development program.” CR-174833, NASA, Washington, DC.
Hunter, G. W. (2003). “Morphing, self-repairing engines: A vision for the intelligent engine of the future.” 2003-3045, American Institute of Aeronautics and Astronautics, Reston, VA.
Hunter, G. W., Jennifer, J. C., and Makel, D. B. (2008). “Case studies in chemical sensor development.” BioNanoFludic MEMS, P. J. Hesketh, ed., Spring Science+Business Media, New York, 197–231.
Hunter, G. W., Setter, J. R., and Hesketh, P. J. (2010). “Smart sensor systems.” Electrochem. Soc. Interface, 19(4), 29–34.
Hunter, G. W., Xu, J. C., Neudeck, P. G., Makel, D. B., and Ward, B. (2006). “Intelligent chemical sensor systems for in-space safety applications.” 06-58419, American Institute of Aeronautics and Astronautics, Reston, VA.
Kaufmann, A. (1963). “Performance of electrical-resistance strain gages at cryogenic temperatures.” TN D-1663, NASA, Washington, DC.
Kemp, R. H., Morgan, W. C., and Manson, S. S. (1947). “The application of high-temperature strain gages to the measurement of vibratory stresses in gas-turbine buckets.” TN-1174, National Advisory Committee for Aeronautics, Washington, DC.
Kemp, R. H., Morse, C. R., and Hirschberg, M. H. (1958). “Application of a high-temperature static strain gage to the measurement of thermal stresses in a turbine stator vane.” TN-4215, National Advisory Committee for Aeronautics, Washington, DC.
Krause, L. N. (1974). “Total-pressure-tube averaging in pulsating flows.” ISA Trans., 13(2), 142–148.
Krause, L. N., and Gettleman, C. C. (1952). “Effect of interaction among probe, supports, duct walls and jet boundaries on pressure measurements in ducts and jets.” ISA Proc., 7, 138–141.
Krause, L. N., Johnson, R. C., and Glawe, G. E. (1958). “A cooled gas pyrometer for use in high temperature gas streams.” TN-4838, National Advisory Committee for Aeronautics, Washington, DC.
Larkin, D. J. (1997). “SiC dopant incorporation control using site-competition CVD.” Phys. Status Solidi B, 202(1), 305–320.
Larkin, D. J., Neudeck, P. G., Powell, J. A., and Matus, L. G. (1994). “Site-competition epitaxy for superior silicon carbide electronics.” Appl. Phys. Lett., 65(13), 1659.
Lei, J. F. (1990). “A resistance strain gage with repeatable and cancelable apparent strain for use to 800°C.” CR-185256, NASA, Washington, DC.
Lei, J. F. (1992). “Palladium-chromium static strain gages for high temperatures.” CP-3161, NASA, Washington, DC, 189–209.
Lei, J. F., and Will, H. A. (1998). “Thin-film thermocouples and strain-gage technologies for engine applications.” Sens. Actuators A Phys., 65(2–3), 187–193.
Lei, J. F., and Williams, W. D. (1990). “PdCr based high temperature static strain gage.” 90-5236, American Institute of Aeronautics and Astronautics, Reston, VA.
Liebert, C. H., Hatch, J. E., and Grant, R. W. (1960). “Application of various techniques for determining local heat-transfer coefficients in a rocket engine from transient experimental data.” TN D-277, NASA, Washington, DC.
Martin, L. C., and Holanda, R. (1994). “Applications of thin film thermocouples for surface temperature measurement.” TM-106714, NASA, Washington, DC.
NASA. (1940). Memorandum, Jun. 11, 1940, National Archives, Record Group 255, Lewis Research Authorization 123.22.
Neudeck, P. G. (2007). “SiC technology.” The VLSI handbook, 2nd Ed., W. -K. Chen, ed., CRC Press, Boca Raton, FL, 5.1–5.34.
Neudeck, P. G., et al. (2008). “Stable electrical operation of 6H-SiC JFETs and ICs for thousands of hours at 500°C.” IEEE Electron Device Lett., 29(5), 456–459.
Neudeck, P. G., et al. (2009). “Extreme temperature 6H-SiC JFET integrated circuit technology.” Phys. Status Solidi A, 206(10), 2329–2345.
Neudeck, P. G., Chen, L. Y., Krasowski, M. J., and Prokop, N. F. (2010). “Characterization of 6H-SiC JFET integrated circuits over a broad temperature range from –150°C to +500°C.” Silicon carbide and related materials: 2009 (Materials Science Forum Volumes 645–648), A. J. Bauer, P. Friedrichs, M. Krieger, G. Pensl, R. Rupp, and T. Seyller, eds., Trans Tech Publications, Stäfa-Zuerich, Switzerland, 1135–1138.
Neudeck, P. G., Okojie, R. S., and Chen, L. Y. (2002). “High-temperature electronics—A role for wide bandgap semiconductors?” Proc. IEEE, 90(6), 1065–1076.
Nieberding, W. C., and Powell, J. A. (1982). “High temperature electronic requirements in aeropropulsion systems.” IEEE Trans. Ind. Electron., IE–29(2), 103–106.
Nishino, S., Powell, J. A., and Will, H. A. (1983). “Production of large-area single-crystal wafers of cubic sic for semiconductor devices.” Appl. Phys. Lett., 42(5), 460.
Norris, W., Kleppe, J., McPherson, D., and Fralick, G. C. (2005). “The measurement of performance of combustors using passive acoustic methods: Additional results.” 2005-219, American Institute of Aeronautics and Astronautics, Reston, VA.
Nyland, T. W., Englund, D. R., and Anderson, R. C. (1971). “On the dynamics of short pressure probes: Some design factors affecting frequency response.” TN D-6151, NASA, Washington, DC.
Okojie, R. S., Beheim, G. M., Saad, G. J., and Savrun, E. (2001). “Characteristics of a hermetic 6H-SiC pressure sensor at 600°C.” 2001-4652, American Institute of Aeronautics and Astronautics, Reston, VA.
Okojie, R. S., DeLaat, J. C., and Saus, J. S. (2005). “SiC pressure sensor for detection of combustion thermo-acoustic instabilities.” Proc., 13th Int. Conf. on Solid State Sensors, Actuators, and Microsystems, IEEE, Piscataway, NJ, 470–473.
Okojie, R. S., Evans, L. J., Lukco, D., and Morris, J. P. (2010). “A novel tungsten-nickel alloy ohmic contact to SiC at 900°C.” IEEE Electron Device Lett., 31(8), 791–793.
Okojie, R. S., Lukco, D., Chen, L. Y., and Spry, D. J. (2002). “Reliability assessment of Ti/TaSi2/Pt ohmic contacts on SiC after 1000 hours at 600°C.” J. Appl. Phys., 91(10), 6553.
Okojie, R. S., Savrun, E., Nguyen, P., Nguyen, V., and Blaha, C. A. (2004). “Reliability evaluation of direct chip attached silicon carbide pressure transducers.” Proc. IEE Sensors Conf., IEEE, Piscataway, NJ, 635–638.
Scadron, M. D., and Warshawsky, I. (1952). “Experimental determination of time constants and nusselt numbers for bare-wire thermocouples in high velocity air streams and analytic approximation of conduction and radiation errors.” TN-2599, National Advisory Committee for Aeronautics, Washington, DC.
Simmons, F. S., and Glawe, G. E. (1957). “Theory and design of a pneumatic temperature probe and experimental results obtained in a high temperature gas stream.” TN-3893, National Advisory Committee for Aeronautics, Washington, DC.
Sokolowski, D. E., and Ensign, R. E. (1986). “Toward improved durability in advanced combustors and turbines—Progress in the prediction of thermomechanical load.” 86-GT-172, ASME, New York.
Stepka, F. S., and Hickel, R. O. (1956). “Methods for measuring temperatures of thin walled gas-turbine blades.” RM E56G17, National Advisory Committee for Aeronautics, Washington, DC.
Summers, R. L., and Anderson, R. C. (1985). “Integrated exhaust gas analysis system for aircraft turbine engine component testing.” TP-2424, NASA, Washington, DC.
Trunek, A. J., et al. (2012). “Lateral growth expansion of 4H/6H-SiC a/m-plane pseudo fiber crystals by hot wall CVD epitaxy.” Materials science forum, silicon carbide and related materials 2011, R. P. Devaty, M. Dudley, T. P. Chow, and P. G. Neudeck, eds., Trans Tech Publications, Dürnten-Zurich, Switzerland, 33–36.
Warshawsky, I. (1989). “Aerospace instrumentation.” Sensors, a comprehensive survey, Vol. 1, fundamentals and general aspects, T. Grandke, and W. H. Ko, eds., VCH Publishers, New York, 579–602.
Warshawsky, I. (1990). “Foundations of measurement and instrumentation.” RP-1222, NASA, Washington, DC.
Will, H. (1993). “Fabrication of thin film heat flux sensors.” N93-13667, NASA, Washington, DC.
Wilson, S. D., Fralick, G. C., Wrbanek, J. D., and Sayir, A. (2010). “Fabrication and testing of a thin film heat flux sensor for a Stirling converter.” TM-2010-216063, NASA, Washington, DC.
Woodworth, A. A., Neudeck, P. G., Sayir, A., Spry, D. J., Trunek, A. J., and Powell, J. A. (2012). “SiC growth by solvent-laser heated floating zone.” Materials science forum, silicon carbide and related materials 2011, R. P. Devaty, M. Dudley, T. P. Chow, and P. G. Neudeck, eds., Trans Tech Publications, Dürnten-Zurich, Switzerland, 49–52.
Wrbanek, J. D. (2010). NASA GRC sensors and electronics branch. NASA, Washington, DC.
Wrbanek, J. D., and Fralick, G. C. (2006). “Thin film physical sensor instrumentation research and development at NASA Glenn Research Center.” TM-2006-214395, NASA, Washington, DC.
Wrbanek, J. D., Fralick, G. C., Gonzalez, J. M., and Laster, K. L. (2008). “Thin film ceramic strain sensor development for high temperature environments.” TM-2008-215256, NASA, Washington, DC.
Wrbanek, J. D., Fralick, G. C., Martin, L. C., and Blaha, C. A. (2001). “A thin film multifunction sensor for harsh enviornments.” TM-2001-211075, NASA, Washington, DC.
Wrbanek, J. D., Wrbanek, S. Y., Fralick, G. C., and Chen, L. Y. (2007). “Micro-fabricated solid-state radiation detectors for active personal dosimetry.” TM-2007-214674, NASA, Washington, DC.

Information & Authors

Information

Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 26Issue 2April 2013
Pages: 409 - 421

History

Received: Apr 26, 2012
Accepted: Nov 21, 2012
Published online: Mar 15, 2013
Published in print: Apr 1, 2013

Permissions

Request permissions for this article.

Authors

Affiliations

Lawrence G. Matus [email protected]
Chief, Sensors and Electronics Branch, National Aeronautics and Space Administration Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44135. E-mail: [email protected]

Metrics & Citations

Metrics

Citations

Download citation

If you have the appropriate software installed, you can download article citation data to the citation manager of your choice. Simply select your manager software from the list below and click Download.

Cited by

View Options

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Media

Figures

Other

Tables

Share

Share

Copy the content Link

Share with email

Email a colleague

Share